In-fiber beam scanning

ABSTRACT

An in-fiber beam scanning system may comprise an input fiber to provide a beam, a feeding fiber comprising an imaging bundle with multiple cores embedded in a first cladding that is surrounded by a second cladding, and an in-fiber beam shifter that comprises a first multibend beam shifter coupled to the input fiber, a graded index fiber following the first multibend beam shifter, and a second multibend beam shifter following the graded index fiber and coupling into the feeding fiber. In some implementations, the first multibend beam shifter is actuated by a first amount and the second multibend beam shifter is actuated by a second amount to shift the beam in two dimensions and deliver the beam into one or more target cores in the imaging bundle.

CROSS-REFERENCE TO RELATED APPLICATION

This Patent Application claims priority to U.S. Provisional Pat. Application No. 63/261,905, filed on Sep. 30, 2021, and entitled “IN-FIBER BEAM SCANNING.” The disclosure of the prior Application is considered part of and incorporated by reference into this Patent Application.

TECHNICAL FIELD

The present disclosure generally relates to steering or otherwise routing an optical beam through a graded index fiber with a set of bends that have a bend period matched to or nearly matched to a pitch of the graded index fiber, and more particularly, to an all-fiber beam routing system utilizing a bent graded index fiber to controllably illuminate different cores in an imaging fiber bundle that includes multiple cores arranged in an array.

BACKGROUND

Laser material processing can be used for cutting, drilling, welding, brazing, surface annealing, alloying, hardening, and/or other applications. In particular, laser material processing generally includes using one or more optical fibers to deliver a high-power and/or high-intensity laser beam to a workpiece on which the laser material processing is to be performed. For example, a typical fiber-delivered laser material processing system may include a laser source (e.g., one or more fiber laser modules), an optical coupler unit, a delivery fiber (typically 10-50 meters in length and included in a delivery cable that may be pluggable on one or both ends), and a processing head. The processing head is an optical assembly that includes a receptacle for the delivery fiber, optics for projecting the laser power, and any components needed for laser-based processing. In operation, the laser source transmits a laser light emission into the optical coupler unit (e.g., through free space or through a separate optical fiber), and the optical coupler unit, which may internally transmit the emission through optical fiber or through free space, and which may magnify or de-magnify the emission, couples the laser light emission into the delivery fiber. The delivery fiber then transmits the laser light to the processing head, which projects the laser light onto a workpiece in association with performing the material processing task. Accordingly, advantages of laser material processing may include high productivity, a noncontact nature of processing, improved quality, and/or a high precision and mobility of a delivery point of the laser beam, among other examples.

One challenge that arises in the context of laser material processing relates to fiber beam shaping (e.g., for cutting, welding, and/or other applications), which is an increasingly important aspect of high-power laser material processing. For example, in some cases, the high power and excellent beam quality of fiber lasers may be leveraged to perform “keyhole welding” with high aspect ratio penetration profiles in narrow fusion zones with low distortion and minimal heat-affected zones. In other examples, a larger laser spot size with a lower power density can be used to perform shallower “conduction welding” that may be used for aesthetic welds and/or minimizing a need for post-processing steps. In still other examples, processing different materials, or materials with different thicknesses, may require different properties in an optical beam (e.g., a high-brightness, small spot size may be desired for some materials, while other materials may require a larger, higher-divergence beam). Accordingly, a laser system with beam shaping capabilities and capabilities to cycle or otherwise transition among multiple states in order to control and/or vary the properties of an optical beam may be desirable.

SUMMARY

In some implementations, an optical assembly includes an input fiber to provide a beam; a feeding fiber comprising an imaging bundle with multiple cores embedded in a first cladding that is surrounded by a second cladding; and an in-fiber beam shifter that comprises a first multibend beam shifter coupled to the input fiber, a graded index fiber following the first multibend beam shifter, and a second multibend beam shifter following the graded index fiber and coupling into the feeding fiber, wherein the first multibend beam shifter is actuated by a first amount and the second multibend beam shifter is actuated by a second amount to shift the beam in two dimensions and deliver the beam into one or more target cores in the imaging bundle.

In some implementations, a method includes providing a beam from an input fiber to an in-fiber beam shifter, wherein the in-fiber beam shifter comprises a first multibend beam shifter coupled to the input fiber, a graded index fiber following the first multibend beam shifter, and a second multibend beam shifter following the graded index fiber and coupling into a feeding fiber, and wherein the feeding fiber comprises an imaging bundle with multiple cores embedded in a first cladding that is surrounded by a second cladding; actuating the first multibend beam shifter by a first amount to shift the beam along a first spatial axis; and actuating the second multibend beam shifter by a second amount to shift the beam along a second spatial axis, wherein the first multibend beam shifter and the second multibend beam shifter are actuated to control Cartesian coordinates representing a position of the beam in two dimensions and to deliver the beam into one or more target cores in the imaging bundle.

In some implementations, an optical assembly includes an input fiber to provide a beam; a feeding fiber comprising multiple cores that are arranged in an array and embedded in a first cladding that is surrounded by a second cladding; and an in-fiber beam shifter that comprises a multibend beam shifter and a graded index fiber coupled between the input fiber and the feeding fiber, wherein the multibend beam shifter is actuated to apply, in the graded index fiber, a set of bends to shift the beam in a spatial dimension and deliver the beam into one or more target cores in the imaging bundle.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a diagram of a graded index fiber.

FIG. 2 is a diagram of one or more example implementations of a bending device that can be used to apply one or more bends in a graded index fiber.

FIG. 3 is a diagram of one or more example implementations of multiple bending devices arranged in a cascaded configuration.

FIGS. 4A-4C are example plots related to a propagation length of a graded index fiber manipulated using bending devices and methods described herein.

FIG. 5 is a flowchart of an example process for applying a set of bends in a graded index fiber using one or more bending devices.

FIGS. 6A-6C are diagrams of one or more example implementations of an all-fiber beam routing system utilizing a bent graded index fiber to controllably illuminate different cores in an imaging fiber bundle that includes multiple cores arranged in an array.

DETAILED DESCRIPTION

The following detailed description of example implementations refers to the accompanying drawings. The same reference numbers in different drawings may identify the same or similar elements.

As described above, fiber beam shaping is an increasingly important aspect of high-power (e.g., greater than 100 watts (W)) laser material processing and/or other applications where a rasterable fiber source may be desirable (e.g., light detection and ranging (LIDAR) and/or endoscopic microscopy, among other examples). For example, a laser that can control and vary beam properties is desirable in the context of laser material processing because different materials, materials with different thicknesses, and/or different material processing techniques may require different properties in an optical beam. For example, a high-brightness, small spot is generally desired for thin stainless steel (e.g., stainless steel with a thickness of less than 3 millimeters (mm)), whereas a larger, higher-divergence beam may be desired for thicker mild steel (e.g., steel with a thickness of more than 12 mm). Additionally, or alternatively, in some applications there may be a desire to create an addressable beam position. For example, in a laser material processing system using a standard imaging (e.g., non-scanning) process head, an addressable beam position may be desired to controllably illuminate different cores in a fiber bundle such that a scannable laser beam can be delivered to a workpiece. However, existing techniques are typically configured to illuminate different cores in a fiber bundle in free space using a coupler box with moving optics, which tends to be more expensive and less reliable than beam scanning techniques that are performed entirely in-fiber. An addressable beam position can be created in a process head by use of high speed scanning mirrors, but this technique adds cost and complexity, and requires a more advanced process head.

Accordingly, an important factor in designing a laser system with beam shaping and/or beam routing capabilities is to provide the ability to cycle or otherwise transition among multiple states that produce optical beams with different properties and/or cause an optical beam to be arbitrarily displaced in one or more dimensions. However, an actuation method is needed to toggle among the different states, which presents a challenge for kilowatt (kW) lasers because the actuation method must be essentially lossless. For example, switches used in telecom and/or datacom applications can incur 0.5 decibels (dB) of loss or more, which is unacceptable for such high powers. The need to provide a lossless actuation method to toggle among different states, in addition to the desirability of keeping the entire system in-fiber for improved manufacturability and reduced alignment tolerances, greatly restricts possible actuation options. Although one simple actuation approach may be to have two laser engines that can be independently turned on and off, this actuation approach significantly increases system cost.

Graded index fibers present one possible alternative to having two independently controlled laser engines. In particular, a graded index fiber generally has a refractive index profile, a square of which is parabolic or near-parabolic, as shown in the following expression:

$n^{2} = n_{1}^{2} - \frac{r^{2}}{f^{2}};r \leq r_{clad}$

where n₁ is a peak (or maximum) refractive index, r is a radial coordinate (e.g., a distance from a center of the graded index fiber), and ƒ is a focal length of the graded index fiber, as related to a pitch of the graded index fiber. Accordingly, bending a graded index fiber generally results in a translation of the beam center, proportional to the curvature of the bend (1/the local bend radius (R_(bend))). The displacement (Δx) is also dependent on properties of the graded index fiber, such as the focal length (ƒ) and the peak/maximum refractive index (n₁) of the graded index fiber, as shown in the following expression:

$\Delta x = \frac{n_{1}^{2}f^{2}}{R_{bend}}$

Thus, one potential method to provide an all-in-fiber beam switch is to use a graded index fiber and bend the graded index fiber adiabatically to varying degrees, such that different beam offset positions inside the fiber can be achieved depending on the curvature of the bend. However, for large offsets, adiabatic bending requires long lengths of bent fiber and large overall bend angles, and may cause significant stress on the fiber, which may lead to breakage. Moreover, if such a shift is desired to achieve a variable-offset launch into a second fiber (e.g., a multicore fiber, a multi-rotary fiber, and/or another suitable fiber), the stress occurs exactly at a splice point, which makes splice optimization more difficult, and makes the splice more prone to failure.

Some implementations described herein relate to a device and method that use a periodic reimaging property of a graded index fiber to route an optical beam within an optical fiber or translate an optical beam in space using a well-controlled series of bends. In this way, by using a series of smaller-strength bends rather than a single long adiabatic bend, some implementations described herein may enable a larger range of beam steering (e.g., relative to a single bend), because large bends may be limited by local stress applied to the optical fiber. Additionally, or alternatively, a single short bend at a well-controlled position (rather than a series of bends) may be formed in the graded index fiber, which may reduce stress on the graded index fiber and reduce the need for the bend apparatus to be precisely tailored to the periodicity or pitch of a particular graded index fiber. Furthermore, by routing the optical beam within an optical fiber, some implementations described herein may eliminate or reduce input/output coupling loss into the routing device and improve manufacturability with reduced alignment tolerances. Additionally, some implementations described herein can be used to route beams in both space and angle, enabling controlled two-dimensional beam steering out of an optical fiber. In some implementations, the device and method described herein may be used in kW fiber beam shaping or in other fields such as LIDAR, endoscopic microscopy, and/or any other suitable application in which a rasterable fiber source may be desirable.

For example, some implementations described herein may be used to manipulate a spatial position of a beam within a fiber in order to deliver a scannable beam to a workpiece via an all-fiber delivery system compatible with standard imaging (e.g., non-scanning) process heads. For example, some implementations described herein relate to an optical assembly that includes two cascaded beam shifters that may be configured to work together to shift a beam an arbitrary amount in a two-dimensional plane before launching the beam into a feeding fiber that includes multiple cores arranged in a two-dimensional array. In this way, the beam may be shifted in two dimensions in order to illuminate different cores in an imaging fiber bundle. Alternatively, in some implementations, a single beam shifter may be used to apply bends in a graded index fiber in any rotational direction about the fiber axis, which may provide radial-coordinate control over the two-dimensional position of the beam. Alternatively, in some implementations, a single beam shifter may be used to displace the beam in one dimension in order to provide a one-dimensional scannable output into a one-dimensional array of cores, which may be useful in applications where a process head is simultaneously moving with respect to a workpiece. Accordingly, as described herein, some implementations relate to an all in-fiber system that can be used to apply a resonant multibend actuator to a graded index fiber and thereby shift a beam in-fiber in one or more dimensions, which may provide an all-fiber delivery system that is compatible with non-scanning process heads in addition to being less expensive and more reliable than systems that rely on coupler boxes with moving optics to enable beam scanning in free space.

FIG. 1 illustrates an example 100 of a graded index fiber. More particularly, as described herein, a square of a refractive index profile of a graded index fiber may be parabolic or near-parabolic (e.g., in a core region), where the refractive index varies smoothly in a radial direction from an axis of the graded index fiber to a certain radial position. In other words, the graded index fiber has a refractive index profile that is parabolic or near-parabolic in cross-section, and uniform along a length of the graded index fiber. Accordingly, light rays that propagate through the graded index fiber follow a periodic trajectory through the parabolic or near-parabolic refractive index profile of the graded index fiber. For example, as shown in FIG. 1 , one or more light rays that originate from a point source (e.g., a laser source and/or an input fiber coupled to a laser source, among other examples) may propagate through the graded index fiber.

Due to periodic imaging properties of the graded index fiber, the point source is exactly reimaged every pitch (and imaged but inverted every half-pitch). Mathematically, the light rays traveling through a single pitch of the graded index fiber are calculated as four successive Fourier transforms, representing collimation (e.g., in a first quarter-pitch), focusing to an inverted image (e.g., in a second quarter-pitch), collimation (e.g., in a third quarter-pitch), and focusing again (e.g., in a fourth quarter-pitch). In some implementations, the pitch of the graded index fiber is determined by a core diameter and a numerical aperture when the graded index fiber is drawn. In some implementations, as described herein, periodic bending of the graded index fiber, with a bend period matched to or nearly matched to a pitch of the graded index fiber, yields a much stronger and more versatile modification of the beam path, compared with adiabatic bending.

As indicated above, FIG. 1 is provided as an example. Other examples may differ from what is described with regard to FIG. 1 .

FIG. 2 is a diagram of one or more example implementations 200 of a bending device 210 that can be used to apply one or more bends in a graded index fiber 215. In some implementations, as described herein, the bending device 210 may be designed to apply a series of bends to the graded index fiber 215 in alternating directions at every odd quarter-pitch (e.g., every half-pitch, starting from a first quarter-pitch) based on the periodic imaging behavior of the graded index fiber 215. In this way, the series of bends may have a bend period that is matched to, or nearly matched to, a pitch of the graded index fiber 215. For example, for a perfect fiber, the period of the bending device 210 would be equal to the pitch of the graded index fiber 215. However, due to fiber manufacturing tolerances, the fabricated pitch can deviate from the nominal value. To correct for the deviation between the fabricated pitch and the nominal value, the bending device 210 may be fabricated to have a period that is shorter than the pitch of the graded index fiber 215, and the bending device 210 may be placed on a goniometer stage 220 (e.g., a device that measures an angle or permits an object to be rotated to a definite position). In some implementations, the goniometer stage 220 may include a knob or other rotation mechanism to rotate the bending device 210 with respect to the graded index fiber 215 in order to elongate the effective period applied to the graded index fiber 215 and enable in-situ adjustments of the period of the perturbations that cause the bends to be formed in the graded index fiber 215.

As described herein, for a given acceptable level of curvature to be imposed on the graded index fiber 215, the bending device 210 may allow a beam to be displaced approximately 4N times farther than using a single adiabatic bend, where N is a number of pitches in the graded index fiber 215. In other words, for a targeted amount of beam offset, the bending device 210 enables the beam offset to be achieved using approximately ¼N times as much bend curvature on the graded index fiber 215. Accordingly, the bending device 210 utilizes the bending properties of the graded index fiber 215 much more effectively than adiabatic bending. In this way, the bending device 210 imposes much less stress on the graded index fiber 215, provides much greater performance, and significantly simplifies mechanical implementation.

As shown in FIG. 2 , the graded index fiber 215, which is nominally N pitches long, is routed through the bending device 210. In some implementations, the bending device 210 has one or more protrusions 235, 245 with a period (A) that is matched to or nearly matched to (e.g., a threshold amount shorter than) a pitch of the graded index fiber 215. At a neutral setting, the protrusions 235, 245 of the bending device 210 are not in contact with the graded index fiber 215 or are barely in contact with the graded index fiber 215. Accordingly, in the neutral setting, the protrusions 235, 245 are exerting no force on the graded index fiber 215. In general, as described above, light launched on-axis at an entrance to the graded index fiber 215 leaves on-axis (Δx = 0), and exactly re-imaged. This fiber state is particularly useful to generate a nominally unperturbed, high-beam-quality output state.

In some implementations, the bending device 210 includes an actuation mechanism 225, such as a micrometer knob and/or another suitable actuator, that may be adjusted to cause a first section 230 of the bending device 210 to move toward a second section 240 of the bending device 210. In some implementations, when the actuation mechanism 225 is adjusted to move the first section 230 toward the second section 240, the protrusions 235, 245 cause the graded index fiber 215 to bend in a wavelike pattern. In some implementations, the bending device 210 may be aligned such that one or more protrusions 235 of the first section 230 and one or more protrusions 245 of the second section 240 align with odd quarter-pitch lengths of the graded index fiber 215. In this way, when the protrusions 235, 245 cause the graded index fiber 215 to bend in the wavelike pattern, a series of bends may be formed in the graded index fiber 215, with a first bend in the series of bends aligned with a first quarter-pitch length of the graded index fiber 215 and each bend in the series of bends spaced a half-pitch length from an adjacent bend. Accordingly, the series of bends that are formed in the graded index fiber 215 are resonant with the intrinsic periodicity of the graded index fiber 215. A small local bend is equivalent to introducing a tilt in the graded index fiber 215, and because the Fourier transform of a tilt is an offset, the resulting effect is that a beam propagating through the graded index fiber 215 is gradually offset from the center of the graded index fiber 215 every half-pitch, as shown by plot 250. The bends (or tilts) that occur every half-pitch are opposite in sign with respect to an axis of the graded index fiber 215, which complements the image-flipping behavior of the graded index fiber 215 every half-pitch and allows the offsets to add constructively. Accordingly, the total offset is controllable by the number of periods of the bending device 210, and how much the two sections 230, 240 of the bending device 210 move toward each other.

In some implementations, configuring the bending device 210 as shown in FIG. 2 may provide a bend with a strength that is independent of the focal length of the graded index fiber 215 to first order. In this way, the graded index fiber 215 can be freely chosen according to other system constraints, such as better mode-matching to an input fiber that is coupled to the graded index fiber 215 to provide a beam to the graded index fiber 215 and/or an output fiber that is coupled to the graded index fiber 215 to receive a beam after traveling through the graded index fiber 215, among other examples. In such cases, the period of the bend apparatus 210 (e.g., a periodicity of the protrusions 235, 245 that cause the bends to be formed in the graded index fiber 215) may be adjusted to correspond to the pitch of the graded index fiber 215. In general, beam-shifting behavior of the bending device 210 is not strongly dependent on the precise shape of the periodic curve induced in the graded index fiber 215. For example, the graded index fiber 215 may be bent in a sinusoidal pattern or another smoothly-varying oscillating curve, an alternating sequence of circular arcs, and/or a sequence of straight or near-straight segments connected by sharp bends near the odd quarter-pitch positions, among other examples. For example, the graded index fiber 215 may have a natural elastic bending shape when bent by near-point-contact actuators as shown in FIG. 2 , which creates a smoothly-varying curve that is close to sinusoidal.

In one numerical example of the bending device 210, an input beam provided by an input fiber may have a spot diameter of 50 microns and a divergence of 0.1 radians. Using a fused-silica graded index fiber 215 with a focal length of 750 microns and a numerical aperture (NA) of 0.21, and accounting for the stress-optic effect induced by the bends in the graded index fiber 215, using four alternating bends (e.g., corresponding to two pitches of the graded index fiber 215, as shown in FIG. 2 ) of 2.4 degrees apiece, spaced by a half-pitch length of 3.5 mm, may generate 100 microns of beam position offset, which is a practical and useful amount in comparison with the actual beam size of 50 microns. The actual bend angle of 2.4 degrees is relatively small and straightforward to actuate upon the graded index fiber 215 without causing damage to the graded index fiber 215 or requiring complicated fiber handling or geometry.

In some implementations, two multi-bend devices 210 can be cascaded, one following the other, with the multi-bend devices 210 oriented in perpendicular orientations with respect to one another (e.g., as shown in FIG. 3 and FIG. 6A and described in further detail below). For example, with an axis of the graded index fiber 210 arranged in a direction z, a first multi-bend device 210 may operate in an x-z plane and a second multi-bend 210 may operate in a y-z plane. Accordingly, the two multi-bend devices 210 may be adjusted independently to allow a user to displace or spatially shift a beam arbitrarily in the x-y plane, which provides a useful capability in many applications where a rasterable or addressable beam position is desired. Additionally, or alternatively, the two-dimensional addressing capability may be realized using a single multi-bend device 210 that can be actuated in any lateral desired direction. For example, the bending device 210 illustrated in FIG. 2 may additionally be rotatable around the fiber axis (e.g., using the rotation mechanism). Additionally, or alternatively, the actuating surfaces that touch the graded index fiber 215 may be small rings or small holes in flat, stacked tabs that can move the graded index fiber 215 in two dimensions at every actuator. The applied motion of the rings or holes may be adjustable in both an x orientation and a y orientation using two-dimensional adjustment stages rather than the one-dimensional stage illustrated in FIG. 2 .

In some implementations, the bending device 210 is made to a high precision, as simulations indicate that the desired deflections are on the order of 10 micrometers (µm). Thus, the protrusions 235, 245 may be fabricated to be precisely the same height, or at least have a precise mirroring relationship between the respective sections. For example, in some implementations, the bending device 210 may be fabricated to a high precision using wire electrical discharge machining and/or other suitable techniques.

As indicated above, FIG. 2 is provided as one or more examples. Other examples may differ from what is described with regard to FIG. 2 . For example, the number and arrangement of components shown in FIG. 2 are provided as an example. In practice, the arrangement shown in FIG. 2 may include additional components, fewer components, different components, or differently arranged components than those shown in FIG. 2 . Additionally, or alternatively, a set of components (e.g., one or more components) in FIG. 2 may perform one or more functions described as being performed by another set of components in FIG. 2 .

FIG. 3 is a diagram of one or more example implementations 300 of multiple bending devices arranged in a cascaded configuration. For example, as shown in FIG. 3 , an input fiber 310 is coupled to a first bending device 320 and a second bending device 330 arranged in a cascaded configuration with a quarter-pitch graded index fiber 340 between the two bending devices 320, 330. In some implementations, the bending devices 320, 330 may work on the same axes, perpendicular axes, or another mutual angle. For example, in FIG. 3 , the bending devices 320, 330 are arranged to work on perpendicular axes. Accordingly, the first bending device 320 may control an angle at which a beam leaves the quarter-pitch graded index fiber 340 in a y direction, and the second bending device 330 may control a spatial offset of the beam in an x direction. Combining the two bending devices 320, 330 with the quarter-pitch graded index fiber 340 between the two bending devices 320, 330 allows for control of both beam offset and beam deflection angle (e.g., near field and far field, respectively) on perpendicular axes, thereby generating skew light rays. If the two bending devices 320, 330 are oriented on the same axis, the two bending devices 320, 330 may generate meridional light rays, again with independent adjustment of both the beam offset and deflection angle. In some implementations, the quarter-pitch graded index fiber 340 between the two bending devices 320, 330 may be the same as in a multi-bend device, or different, and/or the quarter-pitch graded index fiber 340 may include multiple graded index elements that have a net action equivalent to one quarter-pitch graded index element.

In some implementations, the two stages 320, 330 may be combined into one multi-bend device, where the graded index fiber 340 can be bent at every quarter-pitch rather than every odd quarter-pitch. In this case, the odd quarter-pitch bends may adjust the beam offset, and the even quarter-pitch bends may adjust the beam angle, measured from the output end in the event of a total length that is not an integral number of half-pitches. If the odd quarter-pitch bends are oriented perpendicularly to the even ones, then the overall bent fiber shape will be approximately helical and the output light will be skew. On the other hand, the output light will be meridional if the two sets of bends are parallel. With typical quarter-pitch lengths on the order of one (1) mm or less, such a device may require an intricate actuation system, especially if the design objective is to provide full two-dimensional addressability in both the beam offset and beam deflection. Furthermore, in order to provide equal sensitivity for both offset and deflection, the graded index fiber 340 may have a focal length that causes a quarter-pitch beam size to be roughly the same as the size of an input beam provided by the input fiber 310. Accordingly, for beam sizes of interest, the graded index fiber 340 may have a focal length of a few hundred microns. Additionally, or alternatively, the input beam size may be adjusted first (e.g., using a single quarter-pitch graded index fiber of suitable focal strength) to change the beam size to a desired new beam size, and a more preferred focal length of the extended graded index fiber can then be used for the bend array.

In some implementations, as described herein, the bends formed in the graded index fiber 340 may have any periodic bend shape with a bend period equal or approximately equal to a pitch of the graded index fiber 340. In this way, the bends formed in the graded index fiber 340 can be used to manipulate the spatial properties of light carried by the graded index fiber 340. In some implementations, the bending can be two-dimensional (e.g., in the x-z plane, where z is the average propagation direction, such as a simple sinusoid), or the bending can be three-dimensional (e.g., in x, y, and z directions, such as a circular helix, an elliptical helix, and/or a more complicated three-dimensional shape that is periodic in the z direction, among other examples). In some implementations, the bend period can be exactly matched to the pitch of the graded index fiber, or the bend period may be nearly matched to the pitch of the graded index fiber by ± 25%, by ± 10%, by ± 3%, and/or another suitable range. Accordingly, in order to be matched or nearly matched to the pitch of the graded index fiber, a deviation between the bend period and the pitch of the graded index fiber may be required to satisfy (e.g., be less than and/or equal to) a threshold (e.g., ± 10% or less). In some implementations, the bending device can, depending on the bend shape, manipulate the beam in the near field (offset position), the far field (beam pointing direction), or both. In this way, forming bends in the graded index fiber 340 that are matched or nearly matched to the pitch of the graded index fiber 340 provide more versatility than adiabatic bending, which is generally limited to manipulating the near field only.

Furthermore, in some implementations, a single bend may be formed in the graded index fiber 340. In general, when a single bend is used, the single bend is substantially equal to or shorter than a half-pitch of the graded index fiber 340, and the single bend is centered on a position in the graded index fiber 215 at least one-quarter-pitch away from an end of the graded index fiber 215. In such cases, some implementations described herein may enhance the bend effect substantially, compared to adiabatic bending. For example, in some implementations, a spliced assembly may include an input fiber to provide a beam, a graded index fiber that is coupled to the input fiber and one-half pitch in length relative to the imaging pitch length of the graded index fiber, and an output fiber capable of receiving a modified beam position from the graded index fiber, with a bend being applied to the graded index fiber, centered on, and strongest at, the middle of the graded index fiber. In some implementations, the bend may or may not extend into the input and/or output fibers, but may generally be weaker in the input and/or output fibers than in the graded index fibers in order to minimize bend stress applied to the splice points. In this case, the spliced assembly may differ from typical adiabatic-bent fibers because the majority of the bend should be equal in length, or shorter, than a half-pitch of the graded index fiber, which would typically be approximately 1-5 mm, and the strongest bend point would be applied not at the output splice point but approximately one quarter-pitch before the output splice, if the objective is to shift the near field only, similar to the adiabatic bend.

In some implementations, an optical system may include an actuation mechanism that allows a bend shape to be adjusted, thereby enabling at least two states of the output beam (e.g., an unperturbed state and a modified state). However, in the simplest case, a static periodic bend shape may be imparted to the graded index fiber 340 such that a given input state is statically transformed into a different output state (e.g., a different beam position and/or beam pointing direction than the input). One example of such a device may include an all-in-fiber rotary beam generator, where the induced fiber bend shape may be helical, and the output beam may be simultaneously offset from the fiber axis and tilted perpendicular to the offset, developing a skew character and orbital angular momentum. If the graded index fiber 340 were to be spliced to an output step-index or ring-index fiber with a radius matched to the spatial offset and an NA matched to the beam tilt angle, then the offset, skew beam would be captured and maintained in a rotating beam. This static rotary beam generator may be realized in an integrated format by fabricating a fiber preform that includes a graded index core that is offset from the fiber center axis, and spinning the fiber during the draw process so that the offset core actually follows a helical path (even though the outside of the fiber may appear straight). If the helical pitch, as determined by the spin rate relative to the draw rate during the fiber drawing process, equals or nearly equals the graded index pitch, then the helical-core fiber can generate a static lateral offset and beam deflection (e.g., a skew beam carrying orbital angular momentum), which may create an annular, rotary beam when the graded index fiber 340 is coupled into an output fiber (e.g., a step-index or ring fiber) of the appropriate diameter and NA to guide the rotary beam. In this way, some implementations described herein may produce a rotary beam that is compact and simple to manufacture. For example, the structure may be only a few millimeters or centimeters long, would not require tapering, would have a straightforward fiber preform fabrication, and may provide an efficient conversion to a rotary beam in terms of both power and brightness.

In some implementations, different options may be used as actuation mechanisms to provide two or more output states in addition to and/or as alternatives to the actuation mechanisms described above. For example, in some implementations, an actuation mechanism may provide full addressability by controlling a two-dimensional transverse position of the graded index fiber at every half-pitch position, every quarter-pitch position, and/or using an array of micro-manipulators, among other examples. In another example, an actuation mechanism may be arranged to switch between a straight fiber shape and a helical fiber shape by holding the graded index fiber straight and slightly tensioned to provide the straight state, and twisting the graded index fiber while providing slight slack in the tension, such that the graded index fiber adopts a helical state with a pre-determined pitch. In another example, switching between a straight shape and a helical fiber shape may be enabled by twisting the graded index fiber around a second (non-optical) fiber of suitable diameter and stiffness with a predetermined number of turns, and either tensioning the optical fiber while slackening the non-optical fiber to provide the straight fiber state, or slackening the optical fiber while tensioning the non-optical fiber, to force the optical fiber into a helical conformation.

As indicated above, FIG. 3 is provided as one or more examples. Other examples may differ from what is described with regard to FIG. 3 . For example, the number and arrangement of components shown in FIG. 3 are provided as an example. In practice, the arrangement shown in FIG. 3 may include additional components, fewer components, different components, or differently arranged components than those shown in FIG. 3 . Additionally, or alternatively, a set of components (e.g., one or more components) in FIG. 3 may perform one or more functions described as being performed by another set of components in FIG. 3 .

FIGS. 4A-4C illustrate example plots 400, 410, 420 related to a propagation length of a graded index fiber manipulated using one or more bending devices and/or one or more methods described herein. For example, as shown in FIG. 4A, plot 400 illustrates a ray trace within a graded index fiber, showing a single ray propagating near an integral number of pitches. The source NA is 0.1. As shown in FIG. 4B, plot 410 shows a lowest-order linearly polarized fundamental mode (LP01) of a 50 µm and 0.22 NA step index fiber launched into different graded index fibers, which propagates a certain number of pitches. Furthermore, referring to FIG. 4C, plot 420 shows how the “aberrations” of even a perfect graded index fiber affect the beam based on changing a spot size. A higher order mode of the same input fiber propagates through a certain number of pitches in the same graded indexes. Because this mode is less well size-matched to the graded indexes, the higher-order mode experiences more aberrations per pitch and expands faster.

Accordingly, one challenge of the bending devices and methods described herein is to achieve a precise length for the graded index fiber. If the length of the graded index fiber is significantly longer or shorter than an integral number of pitches, the input beam may have a “fuzzed out” image, with power at higher radii, which may incur a penalty in brightness (e.g., an increased beam parameter product (BPP)) when coupled into a delivery fiber. As shown in FIG. 4A, for tight size tolerances of approximately 5 µm, the length tolerance is independent of the graded index fiber focal length, and depends only on the input beam NA. For larger tolerances, the focal length may be a factor, with smaller focal lengths being more forgiving. The most forgiving configuration is to choose a graded index focal length that generates exactly the same spot size in both the near field and the far field (e.g., to size-match the graded index to the input beam). For an input beam radius (w) and a divergence (θ), the appropriate graded index focal length is ƒ = w / θ. In this case, the beam does not change size while propagating (although a shape of the beam may oscillate subtly). In this case, the length of the graded index fiber is not critical, nor is the position of the beginning of the bend array with respect to the beginning of the graded index fiber. However, the period of the bend array is well-matched to the graded index pitch, and the final bend controlled in position relative to the end of the graded index fiber, so that the desired manipulation of the near field and/or the far field is achieved.

Furthermore, an additional design consideration is that graded index “lenses” have aberrations, akin to free space elements. For example, even a graded index fiber with a perfect parabolic refractive index profile does not achieve a precise image every pitch, but rather has small errors that accumulate as more pitches are used. These errors depend strongly on the NA and size of the input beam. For example, if the input is a single fundamental mode in a 50 µm diameter 0.22 NA step index fiber, the input can be almost perfectly reimaged after even 100 pitches in a graded index of the correct focal length, as shown in FIG. 4B. However, choosing a different mode in that input fiber, which has a poorer overlap to a corresponding mode in the graded index fiber, aberration per pitch grows progressively larger, as shown in FIG. 4C, even if the fiber length is chosen perfectly, for the same graded index fibers which maintained the spot size of the LP01 mode group of the input fiber. Generally, for a given input fiber, as the NA increases, the number of graded index pitches before significant aberration occurs will decrease. This is mathematically analogous to using a chain of lenses, each of which has a small amount of spherical aberration. Accordingly, in some implementations, a quantity of pitches in a length of the graded index fiber may be chosen to satisfy a threshold value that is based on one or more metrics related to errors that accumulate per-pitch of the graded index fiber. For example, as shown in FIG. 4C, aberrations significantly increase after a propagation length of approximately ten (10) pitches, whereby the series of bends may be formed in a length of graded index fiber that includes ten or fewer pitches in one example.

In some implementations, the exact length of the graded index fiber may not be an integral number of pitches in applications where maintaining brightness is desired. In some implementations, a device length may be chosen to minimize the spot size, rather than to provide a perfect integral number of pitches (akin to aligning a free space system to the circle of least confusion, as opposed to the paraxial focus). Moreover, dependent on the source, small modifications may be made to the refractive index profile to correct for different aberrations. In this way, the refractive index profile design would not be precisely parabolic, but a slightly different function, while still qualitatively a graded index.

Furthermore, aberration consideration may impact the number of periods of perturbation used. A high NA source may only afford a small number of pitches before the beam “fuzzes out,” while a lower NA source may use more pitches. In addition, the required deflection and tolerance on the micrometer stage may be a factor. In an automated system, the micrometers may be replaced with piezoelectrics or similar, enabling sub-second actuation. Additionally, some implementations described herein may have a mechanism to change the effective length to avoid excessive cleaving and polishing to achieve a precise length (e.g., by using heating, longitudinal stress, compressive stress, and/or other suitable techniques to vary the optical path length).

As indicated above, FIGS. 4A-4C are provided as one or more examples. Other examples may differ from what is described with regard to FIGS. 4A-4C.

FIG. 5 is a flowchart of an example process 500 for applying a set of bends in a graded index fiber using one or more bending devices.

As shown in FIG. 5 , process 500 may include routing a graded index fiber through one or more bending devices, wherein the one or more bending devices comprise one or more protrusions that have a periodicity matched to or nearly matched to a pitch of the graded index fiber (block 510). For example, in some implementations, a graded index fiber 100, 215, 340 may be routed through one or more bending devices 210, 320, 330, as described above. In some implementations, the one or more bending devices 210, 320, 330 comprise one or more protrusions 235, 245 that have a periodicity matched to or nearly matched to a pitch of the graded index fiber 100, 215, 340.

As further shown in FIG. 5 , process 500 may include actuating a first section of the one or more bending devices to move towards a second section of the one or more bending devices such that the one or more protrusions cause a series of bends to be formed in the graded index fiber, wherein the periodicity of the one or more protrusions causes the series of bends to have a bend period matched to or nearly matched to the pitch of the graded index fiber (block 520). For example, in some implementations, a first section 230 of the one or more bending devices 210, 320, 330 may be actuated to move towards a second section 240 of the one or more bending devices 210, 320, 330 such that the one or more protrusions 235, 245 cause a series of bends to be formed in the graded index fiber 100, 215, 340. In some implementations, the periodicity of the one or more protrusions 235, 245 causes the series of bends to have a bend period matched to or nearly matched to the pitch of the graded index fiber 100, 215, 340.

Process 500 may include additional implementations, such as any single implementation or any combination of implementations described below and/or in connection with one or more other processes and/or implementations described elsewhere herein.

For example, in a first implementation, the one or more bending devices may comprise a first bending device 320 arranged to cause a first series of bends in the graded index fiber in a first orientation, and a second bending device 330, following the first bending device 320, to cause a second series of bends in the graded index fiber in a second orientation.

In a second implementation, alone or in combination with the first implementation, the first series of bends in the first orientation and the second series of bends in the second orientation may be perpendicular to one another or parallel to one another.

In a third implementation, alone or in combination with one or more of the first and second implementations, the first series of bends manipulate a beam traveling through the graded index fiber in a near field, and the second series of bends manipulate the beam traveling through the graded index fiber in a far field.

In a fourth implementation, alone or in combination with one or more of the first through third implementations, process 500 includes rotating the one or more bending devices with respect to the graded index fiber, where the periodicity of the one or more protrusions is shorter than the pitch of the graded index fiber, and rotating the one or more bending devices with respect to the graded index fiber elongates the bend period to match or to nearly match the bend period to the pitch of the graded index fiber.

In a fifth implementation, alone or in combination with one or more of the first through fourth implementations, the series of bends are formed in the graded index fiber in two dimensions or in three dimensions.

Although FIG. 5 shows example blocks of process 500, in some implementations, process 500 may include additional blocks, fewer blocks, different blocks, or differently arranged blocks than those depicted in FIG. 5 . Additionally, or alternatively, two or more of the blocks of process 500 may be performed in parallel.

FIGS. 6A-6C are diagrams of one or more example implementations 600 of an all-fiber beam routing system utilizing a bent graded index fiber to controllably illuminate different cores in an imaging fiber bundle that includes multiple cores arranged in an array. Accordingly, as described in further detail herein, example implementation(s) 600 may be used to deliver a scannable laser beam to a workpiece via an all-fiber delivery system that is compatible with standard imaging process heads that may otherwise lack beam scanning capabilities. For example, as shown in FIG. 6A, the all-fiber delivery system may include an input fiber 610 coupled to a first multibend beam shifter 620 and a second multibend beam shifter 630 that are arranged in a cascaded configuration with a graded index (GRIN) fiber 640 provided between the two multibend beam shifters 620, 630. In some implementations, the multibend beam shifters 620, 630 may work on the same axes, perpendicular axes, or another mutual angle. For example, in FIG. 6A, the multibend beam shifters 620, 630 are arranged to work on perpendicular axes (shown as multibend in y and multibend in x, respectively). Accordingly, in one example described herein, the first multibend beam shifter 620 may introduce a spatial shift on a first spatial axis (e.g., in an x direction), and the second multibend beam shifter 630 may introduce a spatial shift on a second spatial axis (e.g., in any direction).

In some implementations, as described herein, the cascading configuration shown in FIG. 6A may be used to manipulate the position of a beam within a fiber. Furthermore, in some implementations described herein, the cascading configuration may be used to deliver a scannable beam to a workpiece via an all-fiber delivery system that may be compatible with standard imaging process heads (e.g., non-scanning process heads). For example, a resonant multibend actuator may be applied to the GRIN fiber 640 to shift a beam in the GRIN fiber 640 using a near field shift configuration. In some implementations, as shown, the first multibend beam shifter 620 is followed by a segment of GRIN fiber 640 that includes an integral number (m) of half-pitches, m*HP, which may include the case of zero (0) half-pitches (e.g., m = 0). As further shown in FIG. 6A, the segment of GRIN fiber 640 may be followed by the second multibend beam shifter 630. In some implementations, the second multibend beam shifter 630 may also be configured to introduce a near field shift, but along a different spatial axis than the first multibend beam shifter 620. The two multibend beam shifters 620, 630 may work together to shift the beam an arbitrary amount in a two-dimensional (2D) plane before the beam is launched into a feeding fiber that contains an imaging fiber bundle 650 with multiple cores arranged in an array. Thus, as the two multibend beam shifters 620, 630 are actuated by different amounts, a user can control which core the light leaves at the end of a process fiber, allowing the user to move the beam in two dimensions. Additionally, or alternatively, the same effect may be accomplished using a single multibend actuator that can apply bends in any rotational direction about the fiber axis (e.g., providing radial-coordinate control as opposed to Cartesian control). In some implementations, a standard imaging process head may image the beam displacement to the workpiece. Controlling the beam near field position on the workpiece in this way is equivalent to introducing a 2D spatial beam scanner in the process head by galvanometer mirror systems, rotating prisms, and/or other arrangements that are typically expensive to design and fabricate, in addition to requiring custom process heads.

In some implementations, as described herein, the cores of the imaging fiber bundle 650 may be arranged in an array, which may have any suitable ID or 2D geometry. For example, FIG. 6B illustrates example 2D geometries 650-1, 650-2, 650-3, 650-4, 650-5 in which the cores of the imaging fiber bundle 650 may be arranged. As shown in FIG. 6B, the imaging fiber bundle 650 may generally include a core-in-clad structure, where multiple cores (labelled n1, which denotes a refractive index of the cores) are embedded in a first (inner) cladding (labelled n2, which denotes a refractive index of the inner cladding). As further shown in FIG. 6B, the inner cladding is surrounded by a second (outer) cladding (labelled n3, which denotes a refractive index of the outer cladding). For example, in some implementations, the inner cladding may be surrounded by the outer cladding to prevent light launched between the cores from leaking out of the fiber. Although all of the examples 650-1 through 650-5 show cores having a uniform refractive index (n1) and a uniform size and/or shape embedded in a uniform refractive index cladding (n2), the cores may have different refractive indexes, different sizes, and/or different shapes. In general, however, to ensure guiding within the cores and to avoid loss of power launched between cores, the inequality n3 < n2 < n1 may hold (e.g., the refractive index of the outer cladding material, n3, is less than the refractive index of the inner cladding, n2, which is less than the refractive index of the cores, n1). In some implementations, the cores may be the same or comparably sized relative to the input beam, or the cores may be slightly larger than the input beam to enable the beam to be entirely contained in one core at a time. Alternatively, in some implementations, the cores may be smaller than the input beam, which may allow multiple cores to be populated independently to provide smoother beam motion.

In some implementations, the cores may be packed in the imaging fiber bundle 650 in a way that minimizes the total area of the material making up the inner cladding. For example, in some implementations, the total area of the inner cladding may be minimized by engineering the lattice structure of the core array into a close-packing configuration (e.g., a dense arrangement of congruent circles) and/or by shaping the cores into triangles, squares, hexagons, and/or other shapes. In this way, minimizing the total area of the inner cladding material enables smaller beam shifts, and in the case of a beam simultaneously filling multiple cores, a smaller fraction of light being launched into the cladding material rather than the desired combination of cores. However, in some implementations, the cores may be separated by a minimum distance (e.g., 5 µm) to prevent power from escaping one core into the adjacent core(s) via evanescent effects.

In some implementations, referring again to FIG. 6A, the axes of the multibend beam shifters 620, 630 may correspond to preferential axes of the core lattice in the imaging fiber bundle 650. For example, in the hexagonal packing array shown by example geometry 650-1 in FIG. 6B (e.g., where the circular cores are arranged in a hexagonal pattern), the multibend beam shifters 620, 630 may be oriented such that one multibend beam shifter 620/630 shifts the beam along the horizontal axis, and the other multibend beam shifter 620/630 shifts the beam along a line at sixty (60) degrees to the horizontal axis (e.g., the axes of the multibend beam shifters 620, 630 may correspond to the axes of the basis vectors of the lattice, which define the structure of the imaging fiber bundle 650). Accordingly, in some implementations, the axes of the multibend beam shifters 620, 630 do not need to be perpendicular to each other.

As described elsewhere herein (e.g., above with reference to FIG. 2 ), at a fixed position along a fiber, a multibend beam router will only move a beam in a particular direction with a particular sign. In other words, if the multibend is configured to move the fiber along the x-axis, whether the first bend pushes the fiber in the +x or -x direction will determine whether the beam shifts in the +x or -x direction. Accordingly, in some implementations, the input fiber may be offset spliced, or the core array in the process fiber may be off-center, such that only motion in the +x and +y directions is required to illuminate different cores. Alternatively, the whole multibend apparatus or one side of the multibend apparatus may be movable along the length of the fiber and reconfigurable along a half-pitch of the GRIN fiber 640, to enable a single multibend to move a beam in either the +x or -x direction. Alternatively, the multibend may be configured such that each bend is individually addressable (e.g., by an array of linear actuators or a similar arrangement) or addressable in pairs, sets, or other groupings to achieve the same effect.

In some implementations, referring to FIG. 6C, a scannable beam may be delivered to a workpiece by a single fiber beam shifter (e.g., a resonant multibend or simple non-resonant bender) along one axis launching into a ribbonized fiber bundle or similar fiber with a one-dimensional (1D) core array. In some implementations, the 1D core array may then provide a 1D scannable output, which can be useful in applications where the process head is simultaneously moving with respect to the workpiece (e.g., the 1D scan can impart a transverse “wobble” to a beam being used for cutting or welding). Furthermore, similar to the 2D case described above, the bender may be reconfigurable such that the beam shift is given in either the positive direction or the negative direction along the fiber ribbon. Accordingly, in cases where the cores in the imaging fiber bundle are arranged in a 1D array (e.g., the cores lie along one spatial axis), a single beam shifter 620/630 may act along only one spatial axis (e.g., the spatial axis of the 1D array of cores) to controllably illuminate one or more cores in the 1D array. Alternatively, the 1D core array may be reconfigured into a 2D core array using a fused fiber bundle or the like, translating a 1D beam shift into motion in a plane among different cores in a prescribed sequence or order.

Accordingly, in some implementations, an optical assembly as described herein may comprise an input fiber 610 to provide a beam, a feeding fiber comprising an imaging bundle 650 with multiple cores (labelled n1 in FIG. 6B) embedded in a first cladding (labelled n2 in FIG. 6B) that is surrounded by a second cladding (labelled n3 in FIG. 6B), and an in-fiber beam shifter that comprises a first multibend beam shifter 620 coupled to the input fiber 610, a graded index fiber 640 following the first multibend beam shifter 620, and a second multibend beam shifter 630 following the graded index fiber 640 and coupling into the feeding fiber 650. In some implementations, the first multibend beam shifter 620 is actuated by a first amount and the second multibend beam shifter 630 is actuated by a second amount to shift the beam in two dimensions and deliver the beam into one or more target cores in the imaging bundle 650. For example, the first multibend beam shifter 620 may be actuated by the first amount to shift the beam along a first spatial axis and the second multibend beam shifter 630 may be actuated by the second amount to shift the beam along a second spatial axis, where the first spatial axis and the second spatial axis may correspond to preferential axes of a lattice structure in which the multiple cores are arranged.

In some implementations, the first multibend beam shifter 620 and the second multibend beam shifter 630 are actuated to shift the beam in a near field. In some implementations, a length of the graded index fiber is an integral number of half-pitches, and the multiple cores each have a refractive index that is greater than a refractive index of the first cladding, which is greater than a refractive index of the second cladding. In some implementations, the multiple cores may have a uniform refractive index, a uniform diameter, and/or a uniform shape, or the refractive index, diameter, and/or shape may vary among different cores. In some implementations, the multiple cores may be arranged within the imaging bundle 650 in a 2D array that comprises a lattice structure having a close-packing configuration with a minimum separation between adjacent cores. In some implementations, the multiple cores may have a diameter that is larger than or within a threshold of a diameter of the beam such that the beam is entirely contained in one target core at a time. Alternatively, in some implementations, the multiple cores may have a diameter that is smaller than a diameter of the beam such that the beam can independently populate multiple target cores.

Accordingly, as described herein, an all-fiber beam scanning method may comprise providing a beam from an input fiber 610 to an in-fiber beam shifter that comprises a first multibend beam shifter 620 coupled to the input fiber 610, a graded index fiber 640 following the first multibend beam shifter 620, and a second multibend beam shifter 630 following the graded index fiber 640 and coupling into a feeding fiber. The feeding fiber may comprise an imaging bundle 650 with multiple cores (labelled n1 in FIG. 6B) embedded in a first cladding (labelled n2 in FIG. 6B) that is surrounded by a second cladding (labelled n3 in FIG. 6B). In some implementations, the all-fiber beam scanning method may further comprise actuating the first multibend beam shifter 620 by a first amount to shift the beam along a first spatial axis and actuating the second multibend beam shifter 630 by a second amount to shift the beam along a second spatial axis, where the first multibend beam shifter 620 and the second multibend beam shifter 630 are actuated to control Cartesian coordinates representing a position of the beam in two dimensions and to deliver the beam into one or more target cores in the imaging bundle 650.

Additionally, or alternatively, as described herein, an optical assembly may comprise an input fiber 610 to provide a beam, a feeding fiber comprising multiple cores (labelled n1) that are arranged in an array and embedded in a first cladding (labelled n2) that is surrounded by a second cladding (labelled n3), and an in-fiber beam shifter that comprises a multibend beam shifter 620 and/or 630 and a graded index fiber 640 coupled between the input fiber 610 and the feeding fiber 650. In some implementations, the multibend beam shifter 620/630 may be actuated to apply, in the graded index fiber 640, a set of bends to shift the beam in a spatial dimension and deliver the beam into one or more target cores in the array. For example, in some implementations, the multibend beam shifter 620/630 may be actuated to control radial coordinates representing a position of the beam within the graded index fiber 640 (e.g., a 2D position where the array is a 2D array). Alternatively, in some implementations, the array may be a 1D array in which the multiple cores are arranged along a single spatial axis, whereby a single multibend beam shifter 620/630 shifts the beam along the single spatial axis to illuminate one or more cores in the 1D array.

As indicated above, FIGS. 6A-6C are provided as one or more examples. Other examples may differ from what is described with regard to FIGS. 6A-6C. For example, the number and arrangement of components shown in FIGS. 6A-6C are provided as one or more examples. In practice, the arrangements shown in FIGS. 6A-6C may include additional components, fewer components, different components, or differently arranged components than those shown in FIGS. 6A-6C. Additionally, or alternatively, a set of components (e.g., one or more components) in FIGS. 6A-6C may perform one or more functions described as being performed by another set of components in FIGS. 6A-6C.

The foregoing disclosure provides illustration and description, but is not intended to be exhaustive or to limit the implementations to the precise forms disclosed. Modifications and variations may be made in light of the above disclosure or may be acquired from practice of the implementations. Furthermore, any of the implementations described herein may be combined unless the foregoing disclosure expressly provides a reason that one or more implementations may not be combined.

As used herein, the term “component” is intended to be broadly construed as hardware, firmware, and/or a combination of hardware and software.

Even though particular combinations of features are recited in the claims and/or disclosed in the specification, these combinations are not intended to limit the disclosure of various implementations. In fact, many of these features may be combined in ways not specifically recited in the claims and/or disclosed in the specification. Although each dependent claim listed below may directly depend on only one claim, the disclosure of various implementations includes each dependent claim in combination with every other claim in the claim set. As used herein, a phrase referring to “at least one of” a list of items refers to any combination of those items, including single members. As an example, “at least one of: a, b, or c” is intended to cover a, b, c, a-b, a-c, b-c, and a-b-c, as well as any combination with multiple of the same item.

No element, act, or instruction used herein should be construed as critical or essential unless explicitly described as such. Also, as used herein, the articles “a” and “an” are intended to include one or more items, and may be used interchangeably with “one or more.” Further, as used herein, the article “the” is intended to include one or more items referenced in connection with the article “the” and may be used interchangeably with “the one or more.” Furthermore, as used herein, the term “set” is intended to include one or more items (e.g., related items, unrelated items, or a combination of related and unrelated items), and may be used interchangeably with “one or more.” Where only one item is intended, the phrase “only one” or similar language is used. Also, as used herein, the terms “has,” “have,” “having,” or the like are intended to be open-ended terms. Further, the phrase “based on” is intended to mean “based, at least in part, on” unless explicitly stated otherwise. Also, as used herein, the term “or” is intended to be inclusive when used in a series and may be used interchangeably with “and/or,” unless explicitly stated otherwise (e.g., if used in combination with “either” or “only one of”). Further, spatially relative terms, such as “below,” “lower,” “above,” “upper,” and the like, may be used herein for ease of description to describe one element or feature’s relationship to another element(s) or feature(s) as illustrated in the figures. The spatially relative terms are intended to encompass different orientations of the apparatus, device, and/or element in use or operation in addition to the orientation depicted in the figures. The apparatus may be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein may likewise be interpreted accordingly. 

What is claimed is:
 1. An optical assembly, comprising: an input fiber to provide a beam; a feeding fiber comprising an imaging bundle with multiple cores embedded in a first cladding that is surrounded by a second cladding; and an in-fiber beam shifter that comprises a first multibend beam shifter coupled to the input fiber, a graded index fiber following the first multibend beam shifter, and a second multibend beam shifter following the graded index fiber and coupling into the feeding fiber, wherein the first multibend beam shifter is actuated by a first amount and the second multibend beam shifter is actuated by a second amount to shift the beam in two dimensions and deliver the beam into one or more target cores in the imaging bundle.
 2. The optical assembly of claim 1, wherein the first multibend beam shifter and the second multibend beam shifter are actuated to shift the beam in a near field.
 3. The optical assembly of claim 1, wherein a length of the graded index fiber is an integral number of half-pitches.
 4. The optical assembly of claim 1, wherein the first multibend beam shifter is actuated by the first amount to shift the beam along a first spatial axis and the second multibend beam shifter is actuated by the second amount to shift the beam along a second spatial axis.
 5. The optical assembly of claim 4, wherein the first spatial axis and the second spatial axis correspond to preferential axes of a lattice structure in which the multiple cores are arranged.
 6. The optical assembly of claim 1, wherein the multiple cores each have a refractive index that is greater than a refractive index of the first cladding, and wherein the refractive index of the first cladding is greater than a refractive index of the second cladding.
 7. The optical assembly of claim 1, wherein the multiple cores have one or more of a uniform refractive index, a uniform diameter, or a uniform shape.
 8. The optical assembly of claim 1, wherein the multiple cores are arranged within the imaging bundle in a two-dimensional array.
 9. The optical assembly of claim 8, wherein the two-dimensional array comprises a lattice structure having a close-packing configuration with a minimum separation between adjacent cores.
 10. The optical assembly of claim 1, wherein the multiple cores have a diameter that is larger than or within a threshold of a diameter of the beam such that the beam is entirely contained in one target core at a time.
 11. The optical assembly of claim 1, wherein the multiple cores have a diameter that is smaller than a diameter of the beam such that the beam can independently populate multiple target cores.
 12. The optical assembly of claim 1, wherein the graded index fiber has a refractive index profile that causes the beam to be re-imaged in the graded index fiber with a bend period having a pitch length, and wherein the graded index fiber comprises a set of bends that have a bend period matched to or nearly matched to the pitch length of the graded index fiber.
 13. A method, comprising: providing a beam from an input fiber to an in-fiber beam shifter, wherein the in-fiber beam shifter comprises a first multibend beam shifter coupled to the input fiber, a graded index fiber following the first multibend beam shifter, and a second multibend beam shifter following the graded index fiber and coupling into a feeding fiber, and wherein the feeding fiber comprises an imaging bundle with multiple cores embedded in a first cladding that is surrounded by a second cladding; actuating the first multibend beam shifter by a first amount to shift the beam along a first spatial axis; and actuating the second multibend beam shifter by a second amount to shift the beam along a second spatial axis, wherein the first multibend beam shifter and the second multibend beam shifter are actuated to control Cartesian coordinates representing a position of the beam in two dimensions and to deliver the beam into one or more target cores in the imaging bundle.
 14. The method of claim 13, wherein the first multibend beam shifter and the second multibend beam shifter are actuated to shift the beam in a near field.
 15. The method of claim 13, wherein the graded index fiber is an integral number of half-pitches.
 16. The method of claim 13, wherein the multiple cores each have a refractive index that is greater than a refractive index of the first cladding, and wherein the refractive index of the first cladding is greater than a refractive index of the second cladding.
 17. The method of claim 13, wherein the multiple cores are arranged within the imaging bundle in a two-dimensional array that comprises a lattice structure having a close-packing configuration with a minimum separation between adjacent cores.
 18. An optical assembly, comprising: an input fiber to provide a beam; a feeding fiber comprising multiple cores that are arranged in an array and embedded in a first cladding that is surrounded by a second cladding; and an in-fiber beam shifter that comprises a multibend beam shifter and a graded index fiber coupled between the input fiber and the feeding fiber, wherein the multibend beam shifter is actuated to apply, in the graded index fiber, a set of bends to shift the beam in a spatial dimension and deliver the beam into one or more target cores in the array.
 19. The optical assembly of claim 18, wherein the multibend beam shifter is actuated to control radial coordinates representing a position of the beam within the graded index fiber.
 20. The optical assembly of claim 18, wherein the array is a one-dimensional array in which the multiple cores are arranged along a single spatial axis. 